The design of maneuvers for Project Galileo is constrained by thruster configuration, modes of thruster usage and limitations required for the safety of the spacecraft and its instruments. The methods used to analyze maneuvers with respect to these constraints is described. The velocity changes necessary for the implementation of a candidate trajectory have been studied and some general conclusions are described.
Constrained maneuver strategies for Project Galileo
1984-08-01
Conference paper
No indication
English
Constrained maneuver strategies for Project Galileo
AIAA | 1984
|Galileo satellite tour maneuver strategies
NTRS | 1978
|Galileo satellite tour maneuver strategies
AIAA | 1978
|NTRS | 1981
|